Aircraft braking method and apparatus

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

Reexamination Certificate

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Details

C701S078000, C701S080000

Reexamination Certificate

active

10517329

ABSTRACT:
An aircraft is decelerated by applying a braking force to a wheel of the aircraft as it moves along the ground. An anti skid controller calculates the braking force to be applied by taking into account data relating to the vertical load transmitted between the ground and the wheel and data relating to the slip between the ground and the wheel. Predictions (box13b) made regarding how the vertical load will change and data (box13a) concerning the relationship between slip and the ground to wheel friction coefficient are both taken into account when calculating the braking force to be applied. Skids may thereby be predicted in advance and may be reduced or even avoided.

REFERENCES:
patent: 2824713 (1958-02-01), Kelley
patent: 3382012 (1968-05-01), Lucien
patent: 3582151 (1971-06-01), Ruof
patent: 4404633 (1983-09-01), Goicoechea
patent: 4613190 (1986-09-01), Johnson
patent: 4958512 (1990-09-01), Johnsen
patent: 5167385 (1992-12-01), Hafner
patent: 5964511 (1999-10-01), Miyazaki
patent: 0 414 715 (1991-03-01), None
patent: 1018548 (1966-01-01), None
patent: 1077636 (1967-08-01), None
patent: WO89/09710 (1989-10-01), None

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